|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/213; 244/198; 244/090.A; 244/045.R|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 11|
An aircraft with swept back wings and spoilers inlaid into the top surface near the tips of the wings. The aircraft also includes an elevator formed in the center back portion of the aircraft, which is also aft of the spoilers. It is aft to allow an auxiliary control in the elevator signal to cancel the unwanted pitch up moment caused by the spoilers only going up and being aft of the center of gravity of the aircraft. Roll is achieved with these spoilers by the direct action of the lift dumping on one side or the other and by taking advantage of the tra...
What is claimed is: 1. A low-observable aircraft, comprising: an integrated fuselage and first and second swept back wings that generally define the aircraft; a first spoiler control surface positioned on a top surface of said first swept back wing; a second spoiler control surface positioned on a top surface of said second swept back wing; a third control surface integrally formed with said integrated fuselage and said first and second swept back wings; and wherein the low-observable aircraft includes no additional control surfaces. 2. The low-obser...